Burning surfaces evolution in solid propellants: a numerical model

A methodology for the solution of the internal physics of solid propellant rocket motors is described. The problem involves the simulation of a burning surface - a dynamically changing interface between the solid propellant and combustion gas phases. Burning surfaces can have complex shapes that cha...

Full description

Saved in:
Bibliographic Details
Main Authors: Joanna Szmelter, P. Ortiz
Format: Default Article
Published: 2007
Online Access:https://hdl.handle.net/2134/4693
Tags: Add Tag
No Tags, Be the first to tag this record!